Flight control indicator for an aircraft, in particular a...

Details Flight control indicator for an aircraft, in particular a... Flight control indicator for an aircraft, in particular a...

2005-06-07

2005-06-07

Nguyen, Tan Q. (Department: 3661)

Data processing: vehicles, navigation, and relative location

Vehicle control, guidance, operation, or indication

Aeronautical vehicle

C701S121000, C244S234000

Reexamination Certificate

active

06904340

ABSTRACT:
Flight control indicator for an aircraft, in particular a transport airplane, intended to supply the thrust generated by at least one engine of the aircraft.The flight control indicator (1) comprises display means (4) which present, on a viewing screen (5), a dial (6) which is graduated in percentage, whose maximum represents the maximum thrust available for the current phase of flight, in the current configuration of the aircraft and for the current anemometric conditions, and which is furnished with characteristic signs (7, 8), whose positions on the dial (6) respectively represent prescribed and actual thrusts which are expressed as a percentage of the maximum thrust.

REFERENCES:
patent: 4083518 (1978-04-01), Garrison et al.
patent: 4536843 (1985-08-01), Lambregts
patent: 5152169 (1992-10-01), Summerfield et al.
patent: 5299765 (1994-04-01), Blechen
patent: 5386954 (1995-02-01), Bissey et al.
patent: 5457634 (1995-10-01), Chakravarty
patent: 5696704 (1997-12-01), Semrau
patent: 2002/0072831 (2002-06-01), Blondel et al.
Preliminary Search Report dated Jan. 21, 2004 with English translation.

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